DESIGN AND CHARACTERIZATION OF MACH 5 FLOW FOR HIGHLY TURBULENT HYPERSONIC TEST FACILITY
AIAA SciTech Forum and Exposition ; 2021 ; Online
2021
Conference paper
English
Mach 5 and Mach 8 hypersonic test facility
AIAA | 1989
|Hypersonic test facility Patent
NTRS | 1967
|Hypersonic test facility Patent
NTRS | 1966
|